H-3 R/B, 61734 (Decayed)
Orbit data source: Space-Track
H-3 R/B, 61734 was space debris in HEO originally from a launch on Mon, 04 Nov 2024 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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61734 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MHI Tobishima
Mission
Decayed spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
2,500 kg wet, 2,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 5.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 H-3 R/B
1 61734U 24198B 25070.08720895 .09976362 -90319-5 19817-2 0 9996
2 61734 24.3177 130.9128 6072748 276.1801 22.0624 4.10114731 3067Epoch: 2025-03-11T02:05Z
TLE epoch observation values (Epoch: 2025-03-11T02:05:34.853Z)
Latitude
0.00001°
Longitude
-69.42943°
Altitude
3,406.636 km
Speed
7.569 km/s
True Right ascension
08h 43m 50s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:20:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,126.791 km
Perigee altitude
98.138 km
Semi-major axis
16,490.601 km
Eccentricity
0.60727
Inclination
24.3177°
RAAN
130.9128°
Arg. of periapsis
276.1801°
True anomaly
83.83761°
Mean anomaly
22.0624°
Eccentric anomaly
47.86443°
Mean motion
1.02492 °/min
Orbital period
351.25 mins
BSTAR
0.0019817
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Other satellites on launch #198 in the year 2024 (2024-11-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.H-3 R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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